Acoustic Performance of Novel Fan Noise Reduction Technologies for a High Bypass Model Turbofan at Simulated Flight Conditions-Reference-Cited by-同舟云学术

Acoustic Performance of Novel Fan Noise Reduction Technologies for a High Bypass Model Turbofan at Simulated Flight Conditions

Published:2009-05-11 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference)
language:
Short-container-title:

Author:

Elliott David¹,Woodward Richard¹,Podboy Gary¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3140

Reference6 articles.

1. Foam-Metal Liner Attenuation of Low-Speed Fan Noise

2. Woodward, Richard P., Fite, E. Brian, and Podboy, Gary G. "Noise Benefits of Rotor Trailing Edge Blowing for a Model Turbofan," AIAA-2007-1241,January,2007.

3. Jeracki, R.J. "Comprehensive Report of Fan Performance from Duct Rake Instrumentation on 1.294 Pressure Ratio, 806 ft/secTipSpeedTurbofanSimulatorModels,"NASA/TM-2006-213863,Feb.2006.

4. Dahl,M.D.,andWoodward,R.P."ComparisonBetweenDesignandInstalledAcousticCharacteristicsoftheNASALewis 9-by15-FootLowSpeedWindTunnelAcousticTreatment,"NASATP-2996,Apr.1990.

5. Dahl, M.D., and Woodward, R.P. "Background Noise Levels Measured In the NASA Lewis 9- by 15-Foot Low Speed WindTunnel,"NASATP-3274,Nov.1992.

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of Over-the-Rotor Liner on Fan Flutter Stability;AIAA Journal;2024-09-02

2. Passive acoustic liners for aero-engine noise control: A review;Mechanics of Advanced Materials and Structures;2024-03-21

3. On the application of a soft-vane cascade model in rotor-stator interaction noise prediction;International Journal of Gas Turbine, Propulsion and Power Systems;2024

4. Three-dimensional effects of cascade perforations on rotor–stator interaction noise;Journal of Fluid Mechanics;2022-11-18

5. On the flow-acoustic coupling of fan blades with over-the-rotor liner;Journal of Fluid Mechanics;2022-05-11